program cowell_mice

< geocentric orbital motion - Cowell's method >


initial UTC epoch       28 Oct 2008 12:20:07.945
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geocentric state vector and orbital elements
(Earth mean equator and equinox of J2000)

        rx (km)                 ry (km)                rz (km)                rmag (km)
 -4.60024974332150e+002  +5.80009883044849e+003  +3.03157787096969e+003  +6.56073424303502e+003  

        vx (kps)                vy (kps)               vz (kps)               vmag (kps)
 -1.07502138833461e+001  -1.52663582373176e+000  +1.30618963497181e+000  +1.09363543669038e+001  


        sma (km)              eccentricity          inclination (deg)         argper (deg)
 +2.09011299577305e+005  +9.68610639961107e-001  +2.85016246930460e+001  +7.54635009776654e+001 

       raan (deg)          true anomaly (deg)         arglat (deg)            period (min)
 +2.08822482582331e+001  +8.20306504311741e-002  +7.55455316280966e+001  +1.58494567659060e+004 


final UTC epoch         02 Nov 2008 11:50:38.120
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selenocentric state vector and orbital elements
(Earth mean equator and equinox of J2000)

        rx (km)                 ry (km)                rz (km)                rmag (km)
 +4.56800059721031e+001  +9.69290870232217e+002  -2.14671211615243e+003  +2.35584047925507e+003  

        vx (kps)                vy (kps)               vz (kps)               vmag (kps)
 -1.95727932786365e+000  -5.58114059364769e-001  +7.88100531001655e-001  +2.18255266087857e+000  


        sma (km)              eccentricity          inclination (deg)         argper (deg)
 -8.15387337633618e+003  +1.23548681359608e+000  +6.59208804625065e+001  +3.14739329736562e+002 

       raan (deg)          true anomaly (deg)         arglat (deg)            period (min)
 +1.85950712816861e+002  +3.11709440298593e+002  +2.66448770035155e+002  +1.66666500000000e+003 


degree of gravity model            8.00
order of gravity model             8.00